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A framework for design and optimization of tapered composite structures. Part I: From individual panel to global blending structure

机译:用于设计和优化锥形复合结构的框架。第一部分:从单个面板到全局混合结构

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摘要

A novel framework to design tapered composite structures is proposed for buckling analysis with multiple manufacturing constraints, with variables dealt with separately at different levels and manufacturing constraints divided and imposed in each step. The framework is based on two techniques a sequential permutation table (SPT) method and a global shared-layer blending (GSLB) method; a design concept is extending from an individual panel to the overall structure by improving its blending property. A problem to design an 18-panel tapered composite structure is adopted to study and validate the proposed framework; a detailed design process is executed step by step to demonstrate the improvements of blending property. Multiple manufacturing constraints are analyzed for the obtained optimal solution, which is also compared with previous studies. The high efficiency of the proposed framework implies its potential for design of large-scale composite structures with complex manufacturing constraints. (C) 2016 Published by Elsevier Ltd.
机译:提出了一种设计锥形复合结构的新颖框架,用于具有多个制造约束条件的屈曲分析,其中变量在不同级别分别处理,并且制造约束条件在每个步骤中进行划分和施加。该框架基于两种技术:顺序排列表(SPT)方法和全局共享层混合(GSLB)方法。通过改善其融合特性,设计理念已从单个面板扩展到整个结构。通过设计18面板渐缩复合结构的问题来研究和验证所提出的框架。详细的设计过程将逐步执行,以演示混合性能的改进。分析了多个制造约束条件以获得最佳解决方案,并将其与以前的研究进行了比较。拟议框架的高效率意味着其具有复杂制造约束的大型复合结构设计的潜力。 (C)2016由Elsevier Ltd.出版

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